View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 05917U 72022A 23151.49485988 .00000238 00000-0 13028-3 0 9992
2 05917 81.2207 288.8841 0030076 230.4823 129.3688 14.08832053627748
| Epoch (UTC): | 31 May 2023 11:52:35 |
| Eccentricity: | 0.0030076 |
| inclination: | 81.2207° |
| perigee height: | 841 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 288.8841° |
| argument of perigee: | 230.4823° |
| revolutions per day: | 14.08832053 |
| mean anomaly at epoch: | 129.3688° |
| orbit number at epoch: | 62774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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